AU585055B2 - Creación de Inventos y Patentes con Inteligencia Artificial

AU585055B2 – Improvements relating to the joining of aircraft skin panels of the sandwich type to frame elements
– Google Patents

AU585055B2 – Improvements relating to the joining of aircraft skin panels of the sandwich type to frame elements
– Google Patents
Improvements relating to the joining of aircraft skin panels of the sandwich type to frame elements

Info

Publication number
AU585055B2

AU585055B2
AU61763/86A
AU6176386A
AU585055B2
AU 585055 B2
AU585055 B2
AU 585055B2
AU 61763/86 A
AU61763/86 A
AU 61763/86A
AU 6176386 A
AU6176386 A
AU 6176386A
AU 585055 B2
AU585055 B2
AU 585055B2
Authority
AU
Australia
Prior art keywords
joining
frame elements
improvements relating
sandwich type
aircraft skin
Prior art date
1985-07-15
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)

Ceased

Application number
AU61763/86A
Other versions

AU6176386A
(en

Inventor
Paul James Jonas
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

Beechcraft Corp

Original Assignee
Beech Aircraft Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
1985-07-15
Filing date
1986-08-22
Publication date
1989-06-08
Family has litigation

First worldwide family litigation filed
litigation
Critical
https://patents.darts-ip.com/?family=25037085&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=AU585055(B2)
«Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.

1986-08-22
Application filed by Beech Aircraft Corp
filed
Critical
Beech Aircraft Corp

1988-02-25
Publication of AU6176386A
publication
Critical
patent/AU6176386A/en

1989-06-08
Application granted
granted
Critical

1989-06-08
Publication of AU585055B2
publication
Critical
patent/AU585055B2/en

2006-08-22
Anticipated expiration
legal-status
Critical

Status
Ceased
legal-status
Critical
Current

Links

Espacenet

Global Dossier

Discuss

Classifications

D—TEXTILES; PAPER

D03—WEAVING

D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS

D03D25/00—Woven fabrics not otherwise provided for

D03D25/005—Three-dimensional woven fabrics

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor

B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding

B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like

B29C65/5007—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like

B29C65/5028—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like being textile in woven or non-woven form

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor

B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding

B29C65/5064—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like of particular form, e.g. being C-shaped, T-shaped

B29C65/5071—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like of particular form, e.g. being C-shaped, T-shaped and being composed by one single element

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor

B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding

B29C65/5085—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like of particular form, e.g. being C-shaped, T-shaped and comprising grooves, e.g. being E-shaped, H-shaped

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C66/00—General aspects of processes or apparatus for joining preformed parts

B29C66/01—General aspects dealing with the joint area or with the area to be joined

B29C66/05—Particular design of joint configurations

B29C66/10—Particular design of joint configurations particular design of the joint cross-sections

B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section

B29C66/112—Single lapped joints

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C66/00—General aspects of processes or apparatus for joining preformed parts

B29C66/01—General aspects dealing with the joint area or with the area to be joined

B29C66/05—Particular design of joint configurations

B29C66/10—Particular design of joint configurations particular design of the joint cross-sections

B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section

B29C66/114—Single butt joints

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C66/00—General aspects of processes or apparatus for joining preformed parts

B29C66/01—General aspects dealing with the joint area or with the area to be joined

B29C66/05—Particular design of joint configurations

B29C66/10—Particular design of joint configurations particular design of the joint cross-sections

B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section

B29C66/114—Single butt joints

B29C66/1142—Single butt to butt joints

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C66/00—General aspects of processes or apparatus for joining preformed parts

B29C66/01—General aspects dealing with the joint area or with the area to be joined

B29C66/05—Particular design of joint configurations

B29C66/10—Particular design of joint configurations particular design of the joint cross-sections

B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections

B29C66/124—Tongue and groove joints

B29C66/1244—Tongue and groove joints characterised by the male part, i.e. the part comprising the tongue

B29C66/12443—Tongue and groove joints characterised by the male part, i.e. the part comprising the tongue having the tongue substantially in the middle

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C66/00—General aspects of processes or apparatus for joining preformed parts

B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces

B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles

B29C66/43—Joining a relatively small portion of the surface of said articles

B29C66/432—Joining a relatively small portion of the surface of said articles for making tubular articles or closed loops, e.g. by joining several sheets ; for making hollow articles or hollow preforms

B29C66/4326—Joining a relatively small portion of the surface of said articles for making tubular articles or closed loops, e.g. by joining several sheets ; for making hollow articles or hollow preforms for making hollow articles or hollow-preforms, e.g. half-shells

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C66/00—General aspects of processes or apparatus for joining preformed parts

B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles

B29C66/43—Joining a relatively small portion of the surface of said articles

B29C66/434—Joining substantially flat articles for forming corner connections, fork connections or cross connections

B29C66/4344—Joining substantially flat articles for forming fork connections, e.g. for making Y-shaped pieces

B29C66/43441—Joining substantially flat articles for forming fork connections, e.g. for making Y-shaped pieces with two right angles, e.g. for making T-shaped pieces, H-shaped pieces

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C66/00—General aspects of processes or apparatus for joining preformed parts

B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles

B29C66/43—Joining a relatively small portion of the surface of said articles

B29C66/434—Joining substantially flat articles for forming corner connections, fork connections or cross connections

B29C66/4346—Joining substantially flat articles for forming cross connections, e.g. for making X-shaped pieces

B29C66/43461—Joining substantially flat articles for forming cross connections, e.g. for making X-shaped pieces with four right angles, e.g. for making +-shaped pieces

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C66/00—General aspects of processes or apparatus for joining preformed parts

B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles

B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles

B29C66/54—Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts

B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics

B29C70/06—Fibrous reinforcements only

B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres

B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length

B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure

B29C70/222—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure being shaped to form a three dimensional configuration

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts

B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics

B29C70/06—Fibrous reinforcements only

B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres

B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length

B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE

B29D24/00—Producing articles with hollow walls

B29D24/002—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled

B29D24/004—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having vertical or oblique ribs

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE

B29D99/00—Subject matter not provided for in other groups of this subclass

B29D99/0003—Producing profiled members, e.g. beams

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE

B29D99/00—Subject matter not provided for in other groups of this subclass

B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings

B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs

B—PERFORMING OPERATIONS; TRANSPORTING

B64—AIRCRAFT; AVIATION; COSMONAUTICS

B64C—AEROPLANES; HELICOPTERS

B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like

B64C1/06—Frames; Stringers; Longerons ; Fuselage sections

B64C1/12—Construction or attachment of skin panels

B—PERFORMING OPERATIONS; TRANSPORTING

B64—AIRCRAFT; AVIATION; COSMONAUTICS

B64C—AEROPLANES; HELICOPTERS

B64C3/00—Wings

B64C3/18—Spars; Ribs; Stringers

D—TEXTILES; PAPER

D03—WEAVING

D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS

D03D11/00—Double or multi-ply fabrics not otherwise provided for

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor

B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding

B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives

B29C65/483—Reactive adhesives, e.g. chemically curing adhesives

B29C65/4835—Heat curing adhesives

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor

B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding

B29C65/5035—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like being in thread form, i.e. in the form of a single filament, e.g. in the form of a single coated filament

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C66/00—General aspects of processes or apparatus for joining preformed parts

B29C66/01—General aspects dealing with the joint area or with the area to be joined

B29C66/05—Particular design of joint configurations

B29C66/10—Particular design of joint configurations particular design of the joint cross-sections

B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections

B29C66/124—Tongue and groove joints

B29C66/1244—Tongue and groove joints characterised by the male part, i.e. the part comprising the tongue

B29C66/12441—Tongue and groove joints characterised by the male part, i.e. the part comprising the tongue being a single wall

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING

B29C66/00—General aspects of processes or apparatus for joining preformed parts

B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material

B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined

B29C66/729—Textile or other fibrous material made from plastics

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES

B29L2024/00—Articles with hollow walls

B29L2024/006—Articles with hollow walls multi-channelled

B—PERFORMING OPERATIONS; TRANSPORTING

B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL

B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES

B29L2031/00—Other particular articles

B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof

B29L2031/3076—Aircrafts

B29L2031/3082—Fuselages

B—PERFORMING OPERATIONS; TRANSPORTING

B64—AIRCRAFT; AVIATION; COSMONAUTICS

B64C—AEROPLANES; HELICOPTERS

B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like

B64C2001/0054—Fuselage structures substantially made from particular materials

B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials

Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS

Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE

Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION

Y02T50/00—Aeronautics or air transport

Y02T50/40—Weight reduction

Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC

Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION

Y10T428/00—Stock material or miscellaneous articles

Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]

Y10T428/24149—Honeycomb-like

AU61763/86A
1985-07-15
1986-08-22
Improvements relating to the joining of aircraft skin panels of the sandwich type to frame elements

Ceased

AU585055B2
(en)

Applications Claiming Priority (1)

Application Number
Priority Date
Filing Date
Title

US06/754,951

US4671470A
(en)

1985-07-15
1985-07-15
Method for fastening aircraft frame elements to sandwich skin panels covering same using woven fiber connectors

Publications (2)

Publication Number
Publication Date

AU6176386A

AU6176386A
(en)

1988-02-25

AU585055B2
true

AU585055B2
(en)

1989-06-08

Family
ID=25037085
Family Applications (1)

Application Number
Title
Priority Date
Filing Date

AU61763/86A
Ceased

AU585055B2
(en)

1985-07-15
1986-08-22
Improvements relating to the joining of aircraft skin panels of the sandwich type to frame elements

Country Status (6)

Country
Link

US
(1)

US4671470A
(en)

EP
(1)

EP0257148B1
(en)

AU
(1)

AU585055B2
(en)

DE
(2)

DE3685586T2
(en)

FR
(1)

FR2603249B1
(en)

GB
(1)

GB2193698B
(en)

Families Citing this family (111)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

FR2602248B1
(en)

1986-08-01
1989-11-24
Brochier Sa

MULTIDIMENSIONAL TEXTILE STRUCTURE FOR REINFORCING LAMINATE MATERIALS AND A WEAVING METHOD AND MATERIAL FOR OBTAINING SUCH A STRUCTURE

US4910065A
(en)

1987-10-15
1990-03-20
The Boeing Company
Reinforced honeycomb core sandwich panels and method for making same

DE68907742T2
(en)

1988-02-19
1993-11-11
Mitsubishi Heavy Ind Ltd

Textile structure for reinforcing structural elements, such as beams, from composite materials and processes for producing the same.

JPH0791725B2
(en)

1988-02-29
1995-10-04
三菱重工業株式会社

Three-dimensional fabric with irregular cross section

US5343897A
(en)

1988-02-29
1994-09-06
Mitsubishi Jukogyo Kabushiki Kaisha
Profiled cross-section three dimensional woven fabric

US5277958A
(en)

1990-01-02
1994-01-11
Tomkins Keith A
Multiple-layer structures and joining method for honeycomb, foam and lightweight materials

US5645744A
(en)

1991-04-05
1997-07-08
The Boeing Company
Retort for achieving thermal uniformity in induction processing of organic matrix composites or metals

US5808281A
(en)

1991-04-05
1998-09-15
The Boeing Company
Multilayer susceptors for achieving thermal uniformity in induction processing of organic matrix composites or metals

US5793024A
(en)

1991-04-05
1998-08-11
The Boeing Company
Bonding using induction heating

US5710414A
(en)

1991-04-05
1998-01-20
The Boeing Company
Internal tooling for induction heating

US5723849A
(en)

1991-04-05
1998-03-03
The Boeing Company
Reinforced susceptor for induction or resistance welding of thermoplastic composites

US7126096B1
(en)

1991-04-05
2006-10-24
Th Boeing Company
Resistance welding of thermoplastics in aerospace structure

US5624594A
(en)

1991-04-05
1997-04-29
The Boeing Company
Fixed coil induction heater for thermoplastic welding

US5500511A
(en)

1991-10-18
1996-03-19
The Boeing Company
Tailored susceptors for induction welding of thermoplastic

FR2687174B1
(en)

1992-02-11
1995-09-22
Aerospatiale

PROCESS FOR THE PRODUCTION OF A FIBER REINFORCEMENT FOR A COMPOSITE MATERIAL WITH NON-COPLANAR WALLS, AND A COMPOSITE PART COMPRISING SUCH A REINFORCEMENT.

DE4417889B4
(en)

1994-05-21
2006-04-13
Burkhart Grob Luft- Und Raumfahrt Gmbh & Co. Kg

Aircraft body and method for its production

US5710412A
(en)

1994-09-28
1998-01-20
The Boeing Company
Fluid tooling for thermoplastic welding

US5660669A
(en)

1994-12-09
1997-08-26
The Boeing Company
Thermoplastic welding

US5573613A
(en)

1995-01-03
1996-11-12
Lunden; C. David
Induction thermometry

US6602810B1
(en)

1995-06-06
2003-08-05
The Boeing Company
Method for alleviating residual tensile strain in thermoplastic welds

US5705795A
(en)

1995-06-06
1998-01-06
The Boeing Company
Gap filling for thermoplastic welds

US5717191A
(en)

1995-06-06
1998-02-10
The Boeing Company
Structural susceptor for thermoplastic welding

US5756973A
(en)

1995-06-07
1998-05-26
The Boeing Company
Barbed susceptor for improviing pulloff strength in welded thermoplastic composite structures

US5829716A
(en)

1995-06-07
1998-11-03
The Boeing Company
Welded aerospace structure using a hybrid metal webbed composite beam

US5657595A
(en)

1995-06-29
1997-08-19
Hexcel-Fyfe Co., L.L.C.
Fabric reinforced beam and column connections

US5760379A
(en)

1995-10-26
1998-06-02
The Boeing Company
Monitoring the bond line temperature in thermoplastic welds

US5786576A
(en)

1995-11-06
1998-07-28
The Boeing Company
Self-steering system for guiding a moving induction coil during thermoplastic welding

US5916469A
(en)

1996-06-06
1999-06-29
The Boeing Company
Susceptor integration into reinforced thermoplastic composites

US5869814A
(en)

1996-07-29
1999-02-09
The Boeing Company
Post-weld annealing of thermoplastic welds

US5902935A
(en)

1996-09-03
1999-05-11
Georgeson; Gary E.
Nondestructive evaluation of composite bonds, especially thermoplastic induction welds

US5698316A
(en)

1996-10-07
1997-12-16
The Boeing Company
Apparatus and methods of providing corrosion resistant conductive path across non conductive joints or gaps

DE19730381C1
(en)

1997-07-16
1998-08-20
Deutsch Zentr Luft & Raumfahrt
Structural element, e.g wing panel for aircraft

US6284089B1
(en)

1997-12-23
2001-09-04
The Boeing Company
Thermoplastic seam welds

US6276866B1
(en)

1998-09-22
2001-08-21
Elbert Rutan
Tensioned structural composite joint

DE19845863B4
(en)

1998-10-05
2005-05-19
Deutsches Zentrum für Luft- und Raumfahrt e.V.

Structural element with large unidirectional stiffness

US6513757B1
(en)

1999-07-19
2003-02-04
Fuji Jukogyo Kabushiki Kaisha
Wing of composite material and method of fabricating the same

US6742547B2
(en)

2000-09-20
2004-06-01
Bally Ribbon Mills
Three-dimensional woven forms with integral bias fibers and bias weaving loom

US6849150B1
(en)

2001-01-16
2005-02-01
Lockheed Martin Corporation
System and method of forming structural assemblies with 3-D woven joint pre-forms

US7521108B2
(en)

2001-05-21
2009-04-21
Lockheed Martin Corporation
Embedded connector attached to a base panel

US6712099B2
(en)

2001-06-15
2004-03-30
Lockheed Martin Corporation
Three-dimensional weave architecture

US6863767B2
(en)

2001-08-23
2005-03-08
Lockheed Martin Corporation
Paste-bond clevis joint

US6676882B2
(en)

2001-08-28
2004-01-13
Lockheed Martin Corporation
Methods of hot-melt resin impregnation of 3-D, woven, textile preforms

WO2003023104A1
(en)

2001-09-12
2003-03-20
Lockheed Martin Corporation
Woven preform for structural joints

US6821368B2
(en)

2001-10-09
2004-11-23
Lockheed Martin Corporation
Co-bonded joint with Z-pins

US20030093964A1
(en)

2001-10-16
2003-05-22
Bushey Richard D.
Floor grid system

US20030116267A1
(en)

2001-12-21
2003-06-26
Sheahen Patrick D.
Low-cost method of assembling structures with 3-D woven connectors

US7238409B1
(en)

2002-05-23
2007-07-03
Rohr, Inc.
Structural element with rib-receiving member

US6945727B2
(en)

2002-07-19
2005-09-20
The Boeing Company
Apparatuses and methods for joining structural members, such as composite structural members

US20040023581A1
(en)

2002-08-05
2004-02-05
Bersuch Larry R.
Z-pin closeout joint and method of assembly

US6749155B2
(en)

2002-09-13
2004-06-15
The Boeing Company
Composite assembly with integrated composite joints

US7197852B2
(en)

2002-09-20
2007-04-03
The Boeing Company
Internally stiffened composite panels and methods for their manufacture

US6871822B2
(en)

2003-04-18
2005-03-29
The Boeing Company
Apparatus and methods of attaching panels to support structures

WO2005106258A1
(en)

2004-04-30
2005-11-10
Indian Institute Of Technology, Bombay
Novel strength enhancing insert assemblies

US7247003B2
(en)

2004-12-02
2007-07-24
Siemens Power Generation, Inc.
Stacked lamellate assembly

US7574835B2
(en)

2005-04-07
2009-08-18
The Boeing Company
Composite-to-metal joint

US7413999B2
(en)

2005-11-03
2008-08-19
Albany Engineered Composites, Inc.
Corner fitting using fiber transfer

FR2896769B1
(en)

2006-01-27
2009-10-09
Eurocopter France

IMPROVED COMPOSITE STRUCTURE FOR AIRCRAFT.

US7887249B2
(en)

2006-06-15
2011-02-15
The Boeing Company
Internal finger joint

US7935205B2
(en)

2006-06-19
2011-05-03
United Technologies Corporation
Repair of composite sandwich structures

US7790294B2
(en)

2006-07-05
2010-09-07
Lockheed Martin Corporation
System, method, and apparatus for three-dimensional woven metal preform structural joint

FR2907800B1
(en)

2006-10-27
2009-03-20
Airbus France Sas

THREE DIMENSIONAL SURFACING WEAVING

US7810757B2
(en)

2006-11-02
2010-10-12
The Boeing Company
Mounting device for an aircraft

US8490362B2
(en)

2007-04-05
2013-07-23
The Boeing Company
Methods and systems for composite structural truss

US7954763B2
(en)

2007-04-05
2011-06-07
The Boeing Company
Methods and systems for composite structural truss

NL1033895C2
(en)

2007-05-25
2008-11-28
Fits Holding B V

Method for manufacturing an object from a sandwich structure with a reinforced angle and such an object.

US8082667B2
(en)

2007-05-31
2011-12-27
The Boeing Company
Apparatus and methods for securing a first structural member and a second structural member to one another

ES2330180B1
(en)

2007-06-28
2010-09-14
Airbus España S.L.

RIGIDIZED MULTILARGUERO TORSION DRAWER.

US8234901B2
(en)

2007-10-25
2012-08-07
The Boeing Company
Method to create bends in composite panels

US8312754B2
(en)

2007-10-25
2012-11-20
The Boeing Company
Method for forming bends in composite panels and composite panels made thereby

US7712488B2
(en)

2008-03-31
2010-05-11
Albany Engineered Composites, Inc.
Fiber architecture for Pi-preforms

US8079549B2
(en)

2008-06-30
2011-12-20
EMBRAER—Empresa Brasileira de Aeronautica S.A.
Monolithic integrated structural panels especially useful for aircraft structures

US8465030B2
(en)

2008-12-07
2013-06-18
Norduyn Inc.
Modular utility cart

US8083489B2
(en)

2009-04-16
2011-12-27
United Technologies Corporation
Hybrid structure fan blade

US8585368B2
(en)

2009-04-16
2013-11-19
United Technologies Corporation
Hybrid structure airfoil

US8992709B2
(en)

2009-12-04
2015-03-31
The Boeing Company
Sandwich structure having arrestment feature and method of making the same

GB201018185D0
(en)

2010-10-28
2010-12-08
Airbus Operations Ltd
Wing tip device attachment apparatus and method

WO2012091695A1
(en)

2010-12-28
2012-07-05
Bell Helicopter Textron Inc.
Multi-directional load joint system

US9016042B2
(en)

2011-05-20
2015-04-28
Rohr, Inc.
Reinforcement members for aircraft propulsion system components configured to address delamination of the inner fixed structure

US8235671B2
(en)

2011-07-19
2012-08-07
General Electric Company
Wind turbine blade shear web connection assembly

US8393871B2
(en)

2011-07-19
2013-03-12
General Electric Company
Wind turbine blade shear web connection assembly

DE102011084438B3
(en)

2011-10-13
2012-11-29
Airbus Operations Gmbh
Producing component for connecting structures at crossing regions of component, comprises depositing first and second fibers on base, connecting them along overlap region, in which first and second fibers overlaps, and pivoting the fibers

DE102011084441A1
(en)

2011-10-13
2013-04-18
Airbus Operations Gmbh

Method for producing a component for connecting structures, components and structural arrangements

DE102011084433A1
(en)

2011-10-13
2013-04-18
Airbus Operations Gmbh

Component, reinforcing member, structure assembly, aircraft or spacecraft and method

DE102011084472B3
(en)

2011-10-13
2013-01-03
Airbus Operations Gmbh
Structural assembly for e.g. aircraft, has fiber section having outer rib in which attachment point is formed so that load applied on attachment point formed in outer rib is transferred by another fiber section to support element

FR2984845B1
(en)

2011-12-21
2014-07-11
Airbus Operations Sas

ANTI-SPEED AIRCRAFT FUSELAGE STRUCTURE ELEMENT

FR2991228B1
(en)

2012-05-29
2015-03-06
Airbus Operations Sas

METHOD AND DEVICE FOR MAKING A SELF-RAIDI COMPOSITE PANEL

US9352822B2
(en)

2012-05-30
2016-05-31
The Boeing Company
Bonded composite airfoil

JP5972702B2
(en)

2012-07-31
2016-08-17
東芝機械株式会社

Machine tool manufacturing method

JP5811082B2
(en)

2012-12-19
2015-11-11
横浜ゴム株式会社

Connection structure for aircraft interior panels

US20140272312A1
(en)

2013-03-13
2014-09-18
Gulfstream Aerospace Corporation
Aircraft component and method of making an aircraft component

EP2783838B1
(en)

2013-03-27
2015-11-18
Airbus Operations GmbH
Composite reinforcement component, structural element, aircraft or spacecraft and method for producing a composite reinforcement component

US9506452B2
(en)

2013-08-28
2016-11-29
General Electric Company
Method for installing a shear web insert within a segmented rotor blade assembly

CA2922198C
(en)

2013-09-04
2021-06-15
Biteam Ab
Method and means for weaving a 3d fabric, 3d fabric items thereof and their use

JP6090931B2
(en)

2013-10-02
2017-03-08
三菱重工業株式会社

Joints and aircraft structures

US9205616B2
(en)

2013-10-11
2015-12-08
The Boeing Company
Bends in composite panels

US9926066B2
(en)

2015-10-14
2018-03-27
The Boeing Company
Corner tension fitting

US10920744B2
(en)

2015-11-26
2021-02-16
Vestas Wind Systems A/S
Manufacture of wind turbine blades

US10570879B2
(en)

2017-05-23
2020-02-25
General Electric Company
Joint assembly for a wind turbine rotor blade with flanged bushings

US10544776B2
(en)

2017-07-27
2020-01-28
General Electric Company
Injection method and device for connecting and repairing a shear web

US10689091B2
(en)

2017-08-02
2020-06-23
Textron Innovations Inc.
Tiltrotor aircraft wings having buckle zones

US10563636B2
(en)

2017-08-07
2020-02-18
General Electric Company
Joint assembly for a wind turbine rotor blade

US10889364B1
(en)

2017-09-15
2021-01-12
Northrop Grumman Systems Corporation
Aircraft full depth pi preform joints

RU2690300C1
(en)

2017-11-09
2019-05-31
Акционерное общество Научно-производственное объединение «Опытно-конструкторское бюро имени М.П. Симонова»
Caisson of wing detachable part

NL2020871B1
(en)

2018-05-03
2019-11-12
Univ Delft Tech
Method for making a virgin joint between two separate structural hollow sections, and such a virgin joint

US11319054B2
(en)

2018-05-31
2022-05-03
Airbus Operations Gmbh
Wing arrangement for an aircraft

US11370526B2
(en)

2018-05-31
2022-06-28
Airbus Operations Gmbh
Latching device for a wing arrangement for an aircraft

US11214353B2
(en)

2018-06-01
2022-01-04
Airbus Operations Gmbh
Wing arrangement for an aircraft and aircraft

EP3587252A1
(en)

2018-06-28
2020-01-01
Airbus Operations GmbH
Arresting system for arresting a first aircraft component relative to a second aircraft component

GB2577936A
(en)

2018-10-12
2020-04-15
Airbus Operations Ltd
Aircraft assembly

US11795831B2
(en)

2020-04-17
2023-10-24
Rtx Corporation
Multi-material vane for a gas turbine engine

US11572796B2
(en)

2020-04-17
2023-02-07
Raytheon Technologies Corporation
Multi-material vane for a gas turbine engine

Citations (2)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

EP0048191A1
(en)

1980-09-09
1982-03-24

Aerospatiale Societe Nationale Industrielle

Airship fuselage structure resistant to longitudinal cracks of the skin

AU1063783A
(en)

1982-02-18
1983-08-25

Stits, R.M.

High tenacity polyester filament fabric

Family Cites Families (10)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

US3090406A
(en)

1961-02-23
1963-05-21
Raymond Dev Ind Inc
Woven panel and method of making same

US3538957A
(en)

1968-08-19
1970-11-10
Hitco
Three-dimensional woven fabric

US3771748A
(en)

1972-10-10
1973-11-13
I M Ind Kynock Ltd
Structures

DE2757965C3
(en)

1977-12-24
1980-07-03
Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen

Thrust transmission element and method for its production

CA1177459A
(en)

1980-04-21
1984-11-06
Lear Fan Corp.
Composite structure for joining intersecting structural members of an airframe and the like

US4565595A
(en)

1981-09-30
1986-01-21
The Boeing Company
Method of making composite aircraft wing

US4395450A
(en)

1981-09-30
1983-07-26
The Boeing Company
Composite structural skin spar joint and method of making

DE3176555D1
(en)

1981-09-30
1988-01-14
Boeing Co
Composite structural skin spar joint and method of making

WO1984004905A1
(en)

1983-06-06
1984-12-20
Boeing Co
Composite aircraft wing and method of making

ATE57398T1
(en)

1986-05-15
1990-10-15
Edo Corp Fiber Science Div

CONNECTION WITH THREE-DIMENSIONAL FABRIC.

1985

1985-07-15
US
US06/754,951
patent/US4671470A/en
not_active
Expired – Lifetime

1986

1986-08-16
GB
GB8620005A
patent/GB2193698B/en
not_active
Expired – Fee Related

1986-08-18
EP
EP86306356A
patent/EP0257148B1/en
not_active
Expired – Lifetime

1986-08-18
DE
DE8686306356T
patent/DE3685586T2/en
not_active
Expired – Fee Related

1986-08-22
AU
AU61763/86A
patent/AU585055B2/en
not_active
Ceased

1986-08-27
FR
FR8612141A
patent/FR2603249B1/en
not_active
Expired

1986-09-02
DE
DE8623542U
patent/DE8623542U1/de
not_active
Expired

Patent Citations (2)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

EP0048191A1
(en)

1980-09-09
1982-03-24
Aerospatiale Societe Nationale Industrielle
Airship fuselage structure resistant to longitudinal cracks of the skin

AU1063783A
(en)

1982-02-18
1983-08-25
Stits, R.M.
High tenacity polyester filament fabric

Also Published As

Publication number
Publication date

DE3685586D1
(en)

1992-07-09

GB2193698A
(en)

1988-02-17

GB2193698B
(en)

1990-09-26

FR2603249B1
(en)

1988-12-09

GB8620005D0
(en)

1986-09-24

EP0257148B1
(en)

1992-06-03

US4671470A
(en)

1987-06-09

FR2603249A1
(en)

1988-03-04

DE3685586T2
(en)

1993-01-21

DE8623542U1
(en)

1988-01-07

EP0257148A1
(en)

1988-03-02

AU6176386A
(en)

1988-02-25

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